EP0875451A3 - Commande de puissance électronique pour aéronef - Google Patents

Commande de puissance électronique pour aéronef Download PDF

Info

Publication number: EP0875451A3
Authority: EP; European Patent Office
Prior art keywords: aircraft; control system; throttle control; electronic throttle; control member
Prior art date: 1997-03-27
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.): Granted

Application number

EP98302370A

Other languages

German (de)

English (en)

Other versions

EP0875451B1 (fr

EP0875451A2 (fr

Inventor

Edward British Aerospace Defence Ltd. Wilson

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

BAE Systems PLC

Original Assignee

British Aerospace PLC

Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)

1997-03-27

Filing date

1998-03-27

Publication date

1999-09-15

1998-03-27 Application filed by British Aerospace PLC filed Critical British Aerospace PLC

1998-11-04 Publication of EP0875451A2 publication Critical patent/EP0875451A2/fr

1999-09-15 Publication of EP0875451A3 publication Critical patent/EP0875451A3/fr

2003-02-19 Application granted granted Critical

2003-02-19 Publication of EP0875451B1 publication Critical patent/EP0875451B1/fr

2018-03-27 Anticipated expiration legal-status Critical

Status Expired - Lifetime legal-status Critical Current

Links

238000001514 detection method Methods 0.000 abstract 1

Classifications

- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/042—Initiating means actuated personally operated by hand

Landscapes

Engineering & Computer Science (AREA)
Automation & Control Theory (AREA)
Aviation & Aerospace Engineering (AREA)
Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
Mechanical Control Devices (AREA)
Control Of Position Or Direction (AREA)
Control Of Electric Motors In General (AREA)

EP98302370A 1997-03-27 1998-03-27 Commande de puissance électronique pour aéronef Expired - Lifetime EP0875451B1 (fr)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
GBGB9706447.1A GB9706447D0 (en)	1997-03-27	1997-03-27	Electronic control apparatus
GB9706447		1997-03-27

Publications (3)

Publication Number	Publication Date
EP0875451A2 EP0875451A2 (fr)	1998-11-04
EP0875451A3 true EP0875451A3 (fr)	1999-09-15
EP0875451B1 EP0875451B1 (fr)	2003-02-19

Family

ID=10810012

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
EP98302370A Expired - Lifetime EP0875451B1 (fr)	1997-03-27	1998-03-27	Commande de puissance électronique pour aéronef

Country Status (5)

Country	Link
US (1)	US6242878B1 (fr)
EP (1)	EP0875451B1 (fr)
DE (1)	DE69811422T2 (fr)
ES (1)	ES2189090T3 (fr)
GB (1)	GB9706447D0 (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE19926800A1 (de) *	1999-06-11	2000-12-14	Wittenstein Gmbh & Co Kg	Vorrichtung zum Steuern eines Triebwerkes
JP2002062944A (ja) *	2000-08-18	2002-02-28	Alps Electric Co Ltd	車載用入力装置
GB0213718D0 (en) *	2002-06-14	2002-07-24	Thales Plc	Apparatus and method of electrical control loading
EP1529252A1 (fr) *	2002-08-07	2005-05-11	Koninklijke Philips Electronics N.V.	Procede et dispositif d'identification des parametres d'un systeme electromecanique
DE10310717A1 (de)	2003-03-10	2004-09-23	Wittenstein Ag	Vorrichtung zum Steuern eines Fahrzeuges
DE10338026B4 (de)	2003-08-19	2006-02-23	Eads Deutschland Gmbh	Kraftgesteuerte Schubhebelvorrichtung zum Einstellen des Triebwerkschubs eines Kampfflugzeugs
WO2006032928A1 (fr) *	2004-04-27	2006-03-30	Bae Systems Plc	Appareil de commande
DE102005017993A1 (de) *	2005-04-19	2006-10-26	Bayerische Motoren Werke Ag	Bedienelement mit Rasterung
FR2892835B1 (fr) *	2005-10-28	2008-01-18	Airbus France Sas	Dispositif de commande de regime-moteur, procede de commande de regime-moteur et aeronef comportant un tel dispositif
FR2912724B1 (fr)	2007-02-19	2009-04-24	Ratier Figeac Soc Par Actions	Commande manuelle de vol d'aeronef
DE102015105787A1 (de)	2015-04-15	2016-10-20	Johann Schwöller	Elektroantrieb für ein Luftfahrzeug und Hybridsystem für ein Luftfahrzeug
TW202608766A (zh) *	2024-05-03	2026-03-01	英商Ｂａｅ系統公營股份有限公司	主動式線性節流閥組件
EP4644254A1 (fr) *	2024-05-03	2025-11-05	BAE SYSTEMS plc	Régulateur de puissance linéaire actif
TW202608767A (zh) *	2024-05-03	2026-03-01	英商Ｂａｅ系統公營股份有限公司	主動式線性節流閥
EP4644236A1 (fr) *	2024-05-03	2025-11-05	BAE SYSTEMS plc	Papillon linéaire actif
TW202608768A (zh) *	2024-05-03	2026-03-01	英商Ｂａｅ系統公營股份有限公司	主動式線性節流閥
EP4644253A1 (fr) *	2024-05-03	2025-11-05	BAE SYSTEMS plc	Ensemble de command des gaz linéaire actif

Citations (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
EP0326439A2 (fr) *	1988-01-29	1989-08-02	British Aerospace Public Limited Company	Dispositif de commande
EP0483773A1 (fr) *	1990-10-29	1992-05-06	Systems Control Technology, Inc.	Dispositif et méthode pour la commande d'une retroaction sur un levier de commande en reponse d'une force y exercée
US5347204A (en) *	1992-10-06	1994-09-13	Honeywell Inc.	Position dependent rate dampening in any active hand controller
FR2708112A1 (fr) *	1993-07-22	1995-01-27	Ratier Figeac Soc	Dispositif de commande à manche de pilotage, notamment mini-manche asservi pour aéronef.
EP0659639A1 (fr) *	1993-12-21	1995-06-28	Honeywell Inc.	Système actif de commande manuelle
US5559415A (en) *	1994-06-30	1996-09-24	Honeywell Inc.	Integrator management for redundant active hand controllers

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US2505555A (en) *	1945-05-21	1950-04-25	Hggins Ind Inc	Mechanical and electrical dual steering system for rudders
US2754465A (en) *	1952-06-07	1956-07-10	Ohio Commw Eng Co	Electric motor control for power steering
US3270260A (en) *	1963-11-18	1966-08-30	Measurement Systems Inc	Stick-operated diaphragm control
US3369161A (en) *	1964-05-07	1968-02-13	Kaman Aircraft Corp	Hard-over attenuation device for servo system
US3854080A (en) *	1973-07-17	1974-12-10	Maurer Commercial Prod Inc	Electrical detenting apparatus
US4150803A (en) *	1977-10-05	1979-04-24	Fernandez Carlos P	Two axes controller
GB2249410B (en) *	1990-10-30	1994-08-03	Rank Cintel Ltd	Control system, especially for film and video tape transport
JP2665313B2 (ja) *	1994-04-22	1997-10-22	国際電業株式会社	反力発生装置

1997
- 1997-03-27 GB GBGB9706447.1A patent/GB9706447D0/en active Pending
1998
- 1998-03-27 ES ES98302370T patent/ES2189090T3/es not_active Expired - Lifetime
- 1998-03-27 DE DE69811422T patent/DE69811422T2/de not_active Expired - Fee Related
- 1998-03-27 EP EP98302370A patent/EP0875451B1/fr not_active Expired - Lifetime
- 1998-03-27 US US09/048,837 patent/US6242878B1/en not_active Expired - Fee Related

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
EP0326439A2 (fr) *	1988-01-29	1989-08-02	British Aerospace Public Limited Company	Dispositif de commande
EP0483773A1 (fr) *	1990-10-29	1992-05-06	Systems Control Technology, Inc.	Dispositif et méthode pour la commande d'une retroaction sur un levier de commande en reponse d'une force y exercée
US5347204A (en) *	1992-10-06	1994-09-13	Honeywell Inc.	Position dependent rate dampening in any active hand controller
FR2708112A1 (fr) *	1993-07-22	1995-01-27	Ratier Figeac Soc	Dispositif de commande à manche de pilotage, notamment mini-manche asservi pour aéronef.
EP0659639A1 (fr) *	1993-12-21	1995-06-28	Honeywell Inc.	Système actif de commande manuelle
US5559415A (en) *	1994-06-30	1996-09-24	Honeywell Inc.	Integrator management for redundant active hand controllers

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
HEGG J W ET AL: "SIDESTICK CONTROLLERS FOR ADVANCED AIRCRAFT COCKPITS", SCIENTIFIC HONEYWELLER, 1 January 1993 (1993-01-01), pages 70 - 77, XP000429070, ISSN: 0196-8440 *

Also Published As

Publication number	Publication date
DE69811422T2 (de)	2003-10-02
GB9706447D0 (en)	1997-10-15
US6242878B1 (en)	2001-06-05
EP0875451B1 (fr)	2003-02-19
EP0875451A2 (fr)	1998-11-04
ES2189090T3 (es)	2003-07-01
DE69811422D1 (de)	2003-03-27

Legal Events

Date	Code	Title	Description
1998-09-18	PUAI	Public reference made under article 153(3) epc to a published international application that has entered the european phase	Free format text: ORIGINAL CODE: 0009012
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1999-07-30	PUAL	Search report despatched	Free format text: ORIGINAL CODE: 0009013
1999-09-15	AK	Designated contracting states	Kind code of ref document: A3 Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE
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1999-09-15	RIC1	Information provided on ipc code assigned before grant	Free format text: 6B 64D 31/02 A, 6B 64C 13/04 B, 6G 05G 5/03 B, 6G 05D 1/00 B
2000-03-29	17P	Request for examination filed	Effective date: 20000128
2000-05-24	AKX	Designation fees paid	Free format text: DE ES FR GB IT
2000-10-18	RAP1	Party data changed (applicant data changed or rights of an application transferred)	Owner name: BAE SYSTEMS PLC
2001-01-17	17Q	First examination report despatched	Effective date: 20001130
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